Browse Topic: Crash prevention
From 2008 to 2021, 48 helicopter accidents have involved Vortex Ring State (VRS) encounters in the United States. For dangerous situations such as VRS encounters and recoveries, Scenario-Based Training (SBT) in flight simulators could supplement flight training, allowing pilots to practice in a safe environment. In this study, we created and tested a proof of concept for scenario-based training in flight simulators, dedicated to VRS-related accident prevention. The goal is to evaluate pilots' awareness, avoidance, detection, and recovery skills during VRS-inducing scenarios. Moreover, this study intends to provide a holistic analysis of VRS encounters and recoveries by examining the situations and factors leading to VRS-related crashes, and to lay out the pilot's decision-making process during the event. For that purpose, a comprehensive set of scenarios was developed based on an analysis of VRS-related accidents from the National Transportation Safety Board (NTSB) database. Overall, the scenarios successfully triggered VRS encounters as well as avoidance actions, providing insight into pilots' behavior in and around VRS conditions.
ABSTRACT
ABSTRACT The advent of multi-rotor, electric VTOL aircraft capable of carrying passengers and providing on-demand personal air transport promises a revolution not only in urban travel, but also in a multitude of other applications which will change the way that a broad range of people carry out their routine work activities. Many of the eVTOL design projects propose to use current ballistic parachute systems in case of any power or control failure; however, any recovery system which (i) gives a Ground Contact Velocity (GCV) of 5 to 7m/s and (ii) will not deploy properly below c. 100 to 150 feet will not be a solution that can satisfy certification requirements for carrying fare-paying passengers above a crowded urban environment. Active VTOL Crash Prevention Ltd (AVCP) is developing a system combining a rapid opening parachute and rocket motors designed to provide a controlled landing at less than 2m/s in any emergency situation.
ABSTRACT The objective of this work is to provide a better understanding of helicopter accidents (rates, trends, and covariates) and to identify areas that deserve careful attention for accident prevention. Several questions were here investigated, including: (1) whether there are differences in accident rates for helicopters with different number of main rotor blades? (2) whether different engine types are associated with different accident rates, controlling for number of blades? And (3) whether there are seasonality effects in helicopter accident rates? To this effect, Record Linkage of two Federal data sources, the FAA civil helicopter registration data and the NTSB accident data, enabled the investigation of these and other questions. First, the accident rates and trend analysis highlighted the safety challenges that continue to face helicopters (significantly worse track record than commercial airlines, passenger cars, and motorcycles). Second, it was found that helicopter accident rates vary by number of rotor blades. Third, one result upended traditional wisdom, which posited that reciprocating engines are associated with higher accident rates; in its stead, it was shown that helicopter accident rates vary with engine type and number of blades, and that turboshaft are associated with significantly higher accident rates than reciprocating engines for the 4-, 5-, and 6-bladed helicopters. Furthermore, it was shown that helicopter accident rates display seasonality effect. Statistical significance and possible confounders for these results were discussed. The issues here examined deserve careful attention from the helicopter community, and several topics were identified as important areas for future work. Any serious effort to improve helicopter safety will entail action on multiple safety levers, including design, operational, and policy/inspection-related ones. All of these actions should be evidence-based, and they will require better helicopter accident investigations and better flight data.
ABSTRACT The objective of this work and its companion article is to provide a better understanding of helicopter accidents and to identify areas that deserve careful attention for improving safety and accident prevention. Three broad questions were here investigated: (1) whether there are safety blind spots in helicopter inspections and any association between inspection time and accidents? (2) whether there are geographic disparities in helicopter accident rates in the U.S. at the regional and state level? And (3) whether there is any association between pilot age and flight experience, and helicopter accident rates? Record Linkage of two Federal data sources, the FAA civil helicopter registration data and the NTSB accident data, enabled the investigation of these and other questions. The main results included the following. First, it was found that there is a clear and significant association between the time of inspection and the accident occurrence, with 10% of all accidents occurring within 4 flight hours of an inspection (all types of inspections). Second, it was found that there are clear and statistically significant geographic disparities in helicopter accident rates in the U. S., both at the regional and state level. Some of the worst-in-class states (e.g., Arkansas, Utah, West Virginia) have helicopter accident rates that are an order of magnitude higher than the best-in-class (e.g., Vermont, Connecticut). Third, it was found that the likelihood of a helicopter pilot to be in an accident is independent of his or her age. Possible confounders were discussed, and hypotheses were proposed as well as recommendations for the FAA and other stakeholders. The end-objective of these recommendations is to improve the safety track record of helicopters, to advance accident prevention, and to reduce their burden of injury, death, and financial losses.
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